公开(公告)号：US20160265553A1

公开(公告)日：2016-09-15

申请号：US14642358

申请日：2015-03-09

Applicant: CATERPILLAR INC.

Inventor： Richard E. ANNATI ,  Gary W. POWERS ,  Jeffrey W. McCORMACK ,  Steven J. O'HARA

IPC: F04D29/62 ,  F04D25/04 ,  F04D17/10

CPC classification number: F04D29/624 ,  F04D17/06 ,  F04D17/10 ,  F04D25/024 ,  F04D29/4206 ,  F04D29/441 ,  F04D29/444 ,  F05D2220/40

Abstract: A compressor housing assembly is disclosed. The compressor housing assembly includes a compressor housing including a compressor housing flange. The compressor housing assembly may include a bearing housing. The bearing housing may include a body portion and a web. The web may extend outward from the body portion to a web end. The bearing housing may also include a bearing housing flange extending radially outward from the web. The compressor housing assembly may also include a clamping plate having a generally annular shape. The clamping plate may abut on the compressor housing flange and the bearing housing flange. In addition, the compressor housing assembly may include a fastener configured to attach the clamping plate to the compressor housing flange and the bearing housing flange.

Abstract translation: 公开了一种压缩机壳体组件。 压缩机壳体组件包括包括压缩机壳体凸缘的压缩机壳体。 压缩机壳体组件可以包括轴承壳体。 轴承壳体可以包括主体部分和腹板。 纤维网可以从主体部分向外延伸到腹板端部。 轴承壳体还可以包括从腹板径向向外延伸的轴承壳体凸缘。 压缩机壳体组件还可以包括具有大致环形形状的夹板。 夹紧板可以抵靠在压缩机壳体凸缘和轴承壳体凸缘上。 此外，压缩机壳体组件可以包括紧固件，其被构造成将夹紧板附接到压缩机壳体凸缘和轴承壳体凸缘。